A mathematical model suitable for real time simulation of the CH-53 helicopter is presented. This model, which is based on modified nonlinear classical rotor theory and nonlinear fuselage aerodynamics, will be used to support terminal-area guidance and navigation studies on a fixed-base simulator. Validation is achieved by comparing the model response with that of a similar aircraft and by a qualitative comparison of the handling characteristics made by experienced pilots.


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    Title :

    A mathematical model of the CH-53 helicopter


    Contributors:

    Publication date :

    1980-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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